Hydraulic Arbor Design

A sealed oil capsule bulges a thin sleeve to grip a part — OD grip (expanding arbor) or ID grip (expansion chuck). Set the charge, read lift, grip pressure, torque and margins.

Updated: 7/4/2026

Arbor type — which surface grips
Same solver either way — the oil joint just sits on the other side of the sleeve. Switching loads the matching stack below (your edits are replaced). Quick start always restores the OD example, even mid-experiment.
The journey: ① pick the grip type above · ② size the stack — your part is the Workpiece / Tool shank row, its fit is the negative-interference joint · ③ set the charge pressure (top of the knob panel) — the grip tile goes green · ④ read Rating A (max pressure, no part in) and Rating B (torque with the part on) in section 3.
1 · Inputs — sizes & materials
Bore
Inner Ø in
0 = solid shaft. Layers stack outward from here.
#1
Outer Øin
Lengthin
Temp°F
inner Ø 0 in
#2
Outer Øin
Lengthin
Temp°F
inner Ø 1.102 in
#3
Outer Øin
Lengthin
Temp°F
inner Ø 1.26 in
Concentric layers, inside → out. Drag the handle to reorder; each layer's inner Ø follows the one below it (shared wall). Edit material properties in the Materials section below.
#1 Carbon steel 1045 (cold-drawn) Ø 0–1.1 in
#2 Alloy steel 4140 (Q&T) Ø 1.1–1.26 in
#3 Steel (E=200 GPa) Ø 1.26–2.36 in
MaterialCategory E (Mpsi)να (ppm/°F) σy (psi)ρ (lb/in³)k (W/m·K)Eₜ (%E)
Carbon & alloy steel
Steel (E=200 GPa)Carbon & alloy steel29.0080.286.536,259.40.350
Steel A36 (structural)Carbon & alloy steel29.0080.266.536,259.40.350
Steel 1018 (cold-drawn)Carbon & alloy steel29.7330.296.553,6640.352
Carbon steel 1045 (cold-drawn)Carbon & alloy steel29.7330.296.38976,8700.350
Alloy steel 4140 (Q&T)Carbon & alloy steel29.7330.296.83394,999.70.342
Alloy steel 4340 (Q&T)Carbon & alloy steel29.7330.296.833124,732.50.344
AISI 4130 (normalized)Carbon & alloy steel29.7330.296.77863,091.40.342.7
AISI 8620 (normalized core, carburizing grade)Carbon & alloy steel29.7330.296.61152,213.60.346.6
AISI 8620 carburized (58-62 HRC case)Carbon & alloy steel29.7330.296.611166,793.40.346.6
AISI 9310 gear steel (carburized, annealed core)Carbon & alloy steel29.7330.296.83365,2670.342.6
AISI 1020 (as-rolled)Carbon & alloy steel29.0080.296.547,862.50.351.9
AISI 1095 spring steel (Q&T, 480C temper)Carbon & alloy steel29.7330.296.333110,228.70.347
AISI 52100 bearing steel (hardened & tempered)Carbon & alloy steel30.4580.296.611250,190.10.346.6
Maraging steel C250 (18Ni, aged)Carbon & alloy steel26.8320.35.611246,564.20.319.7
Maraging steel C300 (18Ni, aged)Carbon & alloy steel27.5570.35.611290,075.50.325.3
Nitralloy 135M (nitriding steel, Q&T core)Carbon & alloy steel29.7330.296.44489,923.40.322
AISI 4150 (Q&T, 540C temper)Carbon & alloy steel27.5570.296.833175,495.70.342
Alloy steel 4140 (45 HRC)Carbon & alloy steel29.7330.296.833181,297.20.342
AerMet 100 (aged)Carbon & alloy steel28.1370.286.111250,045.10.325
Tool steel
Tool steel O1 (hardened)Tool steel29.7330.36.111210,304.70.346
Tool steel A2 (hardened)Tool steel29.4430.295.889220,457.40.326
Tool steel D2 (hardened)Tool steel30.4580.295.778217,556.60.320
Tool steel H13 (hot-work, hardened ~50 HRC)Tool steel30.4580.35.778185,068.20.324.6
Tool steel S7 (shock-resisting, hardened ~54 HRC)Tool steel30.0230.37234,961.10.324.6
Stainless
Stainless 304Stainless27.9920.299.61131,183.10.316
Stainless 316Stainless27.9920.278.88942,060.90.316
Stainless 410 (tempered)Stainless29.0080.295.560,190.70.325
Stainless 17-4 PH H900Stainless28.5720.276169,694.20.318
Stainless 303 (annealed)Stainless27.9920.39.61134,809.10.316.2
Stainless 321 (annealed)Stainless27.9920.279.22229,732.70.316.1
Stainless 347 (annealed)Stainless27.9920.289.22229,732.70.316.3
Stainless 430 (annealed)Stainless29.0080.35.77844,961.70.326.1
Stainless 440C (hardened)Stainless29.0080.285.667275,571.70.324.2
Stainless 2205 duplex (annealed)Stainless27.5570.37.22265,2670.319
Stainless 2507 super-duplex (annealed)Stainless29.0080.37.22279,770.80.317
Stainless 15-5 PH (H1025)Stainless28.4270.2726145,037.70.317.8
Stainless 13-8 Mo PH (H1000)Stainless28.2820.2786204,503.20.312.8
Stainless A286 (aged)Stainless29.0080.319.11195,724.90.312.6
Nitronic 60 (annealed)Stainless26.9770.299.27860,190.70.314.7
Stainless 904L (annealed)Stainless27.5570.38.531,908.30.311.5
Stainless 254 SMO (annealed)Stainless28.2820.39.16743,511.30.313.5
Cast iron
Gray cast iron G3000 brittleCast iron14.5040.265.83330,022.80.350
Ductile iron 65-45-12Cast iron24.5110.2756.44444,961.70.333
Aluminum
Aluminum 6061-T6Aluminum9.9930.3313.11140,030.40.1167
Aluminum 7075-T6Aluminum10.3990.331372,9540.1130
Aluminum 2024-T4Aluminum10.5880.3312.88946,992.20.1121
Aluminum A356-T6 (cast)Aluminum10.5010.3311.94426,9770.1151
Aluminum 6063-T5Aluminum9.9930.331321,030.50.1209
Aluminum 5052-H32Aluminum10.1960.3313.22227,992.30.1138
Aluminum 2017-T4Aluminum10.5010.3313.11140,030.40.1134
Aluminum 7050-T7451Aluminum10.3990.3313.05668,022.70.1157
Aluminum 7475-T651Aluminum10.1960.331367,007.40.1163
Aluminum 6082-T6Aluminum10.1530.3313.33336,259.40.1170
Aluminum 2219-T87Aluminum10.6020.3312.556,999.80.1120
Aluminum 5083-H116Aluminum10.1960.3313.22231,183.10.1117
Aluminum 6005A-T6Aluminum10.0080.3312.77832,633.50.1188
Aluminum MIC-6 cast tooling plateAluminum10.2980.3313.61117,984.70.1142
Copper alloy
Brass C360Copper alloy14.0690.3411.38918,129.70.3115
Bronze C932 (bearing)Copper alloy14.5040.341018,129.70.359
Phosphor bronze C510Copper alloy15.9540.349.88955,114.30.384
Beryllium copper C17200Copper alloy18.5650.39.889159,541.50.3105
Copper C101Copper alloy16.9690.349.44410,152.60.3391
Aluminum bronze C95200 (952)Copper alloy15.9540.32924,656.40.350
Cartridge brass C260 (H02)Copper alloy15.9540.3511.05650,0380.3120
Commercial bronze C220 (H02)Copper alloy16.9690.3310.22244,961.70.3119
Naval brass C464 (O61 annealed)Copper alloy14.5040.3411.77824,656.40.3116
Aluminum bronze C630 (C63000)Copper alloy17.4050.34950,0380.339
Nickel-aluminum bronze C955 (C95500, as-cast)Copper alloy15.9540.32942,060.90.342
Cupronickel 90-10 C706 (C70600, annealed)Copper alloy19.580.329.515,954.20.345
Cupronickel 70-30 C715 (C71500, annealed)Copper alloy21.7560.34920,305.30.329
Manganese bronze C863 (C86300, cast)Copper alloy14.0690.331260,190.70.335
Silicon bronze C655 (C65500, annealed)Copper alloy14.9390.341021,030.50.336
Leaded bronze C937 (C93700, cast)Copper alloy10.9940.331017,984.70.347
Chromium copper C182 (C18200, TH04)Copper alloy16.9690.339.77865,2670.3324
Copper-nickel-tin C72900 (AT, spinodal)Copper alloy21.030.339.11189,923.40.338
Titanium
Titanium Ti-6Al-4VTitanium16.5050.3424.778127,633.20.26.7
Titanium CP Grade 2Titanium15.2290.374.77839,885.40.217
Titanium Grade 1 CP (annealed)Titanium14.9390.344.77824,656.40.216
Titanium Grade 4 CP (annealed)Titanium15.0840.345.38969,618.10.217
Titanium Ti-6Al-4V ELI (Grade 23, annealed)Titanium16.5340.3425.111115,3050.26.7
Titanium Ti-3Al-2.5V (Grade 9, annealed)Titanium15.5190.35.22269,618.10.27.5
Titanium Ti-5Al-2.5Sn (Grade 6, annealed)Titanium15.9540.315.222119,656.10.27.8
Titanium Ti-6Al-2Sn-4Zr-2Mo (6-2-4-2, duplex annealed)Titanium16.5340.324.278124,732.50.27.1
Titanium Ti-15V-3Cr-3Al-3Sn (Beta, solution treated)Titanium11.8930.324.722111,679.10.28.1
Nickel
Inconel 718 (aged)Nickel29.0080.297.222150,114.10.311
Monel 400Nickel26.1070.327.72234,809.10.322
Inconel 625 (annealed)Nickel30.0230.2787.11166,717.40.39.8
Inconel 600 (annealed)Nickel30.0230.297.38942,060.90.314.9
Inconel X-750 (aged)Nickel30.8930.297120,381.30.312
Hastelloy C-276 (annealed)Nickel29.7330.316.22251,488.40.39.9
Waspaloy (aged)Nickel30.6030.36.778115,3050.311
Incoloy 800H (annealed)Nickel28.4270.34829,732.70.311.5
Incoloy 825 (annealed)Nickel28.4270.297.72239,160.20.311.1
Rene 41 (aged)Nickel31.6180.316.722153,7400.39
Nimonic 90 (aged)Nickel30.8930.317.056101,526.40.311.5
MP35N (annealed)Nickel33.7940.37.11160,045.60.311.2
Cobalt alloy
Stellite 6 (cast) brittleCobalt alloy30.3130.36.33378,320.40.314.8
Haynes 188 (annealed)Cobalt alloy33.6490.36.88967,297.50.310.4
L605 / Haynes 25 (annealed)Cobalt alloy32.6330.296.83364,541.80.39.4
Refractory metal
Molybdenum (wrought)Refractory metal46.4120.312.66772,518.90.4138
TZM molybdenum alloy (stress-relieved)Refractory metal47.1370.312.944124,732.50.4126
Tungsten (wrought)Refractory metal59.6110.282.5108,778.30.7173
Tantalum (annealed)Refractory metal26.9770.343.525,961.80.657
Niobium (annealed)Refractory metal15.2290.44.05615,2290.353.7
Light & specialty
Magnesium AZ31BLight & specialty6.5270.3514.44431,908.30.196
Invar 36 (low-α)Light & specialty20.450.290.66740,030.40.310
Tungsten carbide (6% Co) brittleLight & specialty87.0230.222.778435,113.20.586
Magnesium AZ91D (die cast)Light & specialty6.5270.3514.44421,755.70.172.7
Magnesium ZK60A-T5Light & specialty6.5270.2914.44441,335.80.1121
Magnesium WE43B-T6Light & specialty6.3820.271523,931.20.151
Beryllium S-200F (vacuum hot pressed)Light & specialty43.9460.086.27834,809.10.1200
Zirconium 702 (R60702, annealed)Light & specialty14.3590.353.27830,022.80.222
Zinc die-cast Zamak 3 (ASTM AG40A)Light & specialty13.9240.2515.22230,167.90.2113
Lead (chemical/pure, Pb)Light & specialty2.3210.4416.056797.70.435
Tin (pure, Sn)Light & specialty7.2520.3612.2221,740.50.367
Controlled expansion
Kovar (Fe-Ni-Co)Controlled expansion20.0150.3173.05650,0380.317.3
Alloy 42 (Fe-42Ni)Controlled expansion21.4660.292.94436,259.40.310.7
Babbitt / white metal
Babbitt tin-base (AMS 4800)Babbitt / white metal7.6870.3312.7784,351.10.334
Babbitt lead-base (B23 Gr.13)Babbitt / white metal4.2060.3614.4443,335.90.424
Self-lubricating
Sintered bronze SAE 841Self-lubricating7.2520.2710.27811,022.90.230
Sintered iron SAE 863Self-lubricating11.6030.256.94417,404.50.235
Graphalloy (graphite/metal) brittleSelf-lubricating1.8850.22.514,503.80.120
Ceramic
Alumina 96% brittleCeramic43.5110.214.55650,0380.125
Alumina 99.5% brittleCeramic53.9540.224.66754,969.30.135
Silicon carbide (sintered SiC) brittleCeramic59.4650.142.22255,114.30.1125
Silicon nitride (Si3N4) brittleCeramic44.9620.271.833101,526.40.130
Zirconia 3Y-TZP (yttria-stabilized) brittleCeramic30.4580.35.833145,037.70.22.5
Magnesia-PSZ zirconia (Mg-PSZ) brittleCeramic29.7330.35.77894,274.50.22.7
Boron carbide (B4C) brittleCeramic65.2670.182.77858,015.10.135
Aluminum nitride (AlN) brittleCeramic47.8620.242.546,412.10.1170
Silicon (single-crystal) brittleCeramic18.8550.281.44423,931.20.1150
Sapphire (single-crystal Al2O3) brittleCeramic50.0380.272.94458,015.10.142
Macor (machinable glass-ceramic) brittleCeramic9.7030.295.16713,633.50.11.5
Cordierite brittleCeramic10.1530.221.1119,282.40.13
Glass
Fused silica (quartz glass) brittleGlass10.5880.170.3067,5420.11.4
Borosilicate glass (Borofloat 33 / Pyrex) brittleGlass9.2820.21.8063,625.90.11.2
Soda-lime glass brittleGlass10.4430.23514,503.80.11
Composite
Phenolic (linen Garolite LE) brittleComposite1.0440.21012,473.200.3
G-10 / FR-4 (epoxy-glass)Composite2.6110.188.88937,999.90.10.3
Carbon-fiber / epoxy (quasi-isotropic)Composite7.2520.311.66736,114.40.15
Nylon 6/6, 33% glass-filledComposite1.3050.3813.88926,106.800.3
PEEK, 30% carbon-filledComposite3.4810.48.88932,488.50.10.9
Polymer
PEEK (unfilled)Polymer0.5220.3826.11114,503.800.3
Acetal / POM (Delrin)Polymer0.450.3561.1119,427.50.10.3
Nylon 6/6 (dry)Polymer0.4210.3944.44411,60300.3
PTFE (Teflon)Polymer0.0730.46753,625.90.10.3
UHMW-PEPolymer0.1020.4683.3333,045.800.4
HDPEPolymer0.1450.4283.3333,77100.5
Polycarbonate (PC)Polymer0.3340.3737.7788,992.300.2
PEI / Ultem 1000Polymer0.4350.3631.11115,22900.2
PPS (Ryton)Polymer0.4790.3827.77810,152.600.3
PVDF (Kynar)Polymer0.2470.472.2227,251.90.10.2
Polyimide (Vespel SP-1)Polymer0.450.413012,473.20.10.4
Nylon 6 (cast, dry)Polymer0.4790.444.44412,183.200.3
PET (Ertalyte)Polymer0.450.433.33312,328.20.10.3
Polypropylene (PP)Polymer0.2030.42504,786.200.2
PMMA / acrylic brittlePolymer0.4640.3738.88910,152.600.2
Polysulfone (PSU / Udel)Polymer0.3630.3731.11110,152.600.3
Built-in grades are read-only — click to make an editable copy. Custom materials persist in your browser and are selectable per layer above.

2 · Analysis — turn the knobs, watch it respond

Min SF
3.24
Peak von Mises
29,344.1 psi
Contact p
1,879.4 psi
Assembly force
1,405.7 lbf
Holding torque
73.8 ft·lbf
Axial strain εz
0 µε

Min safety factor: 3.24  ·  Max von Mises: 29,344.1 psi  ·  axial strain εz = 0 µε (free ends, net axial force = 0)

Stress through the wall (radius spans every layer). Drag any knob → the gauges and graph update live.

Response — Sleeve lift ΔØ (in) vs Charge pressure (sealed at assembly) · Joint 1

Grab a knob — this sweeps it across its range; the dashed line marks where you are now.

Hydraulic expansion — sealed capsule
psi
Sealed capsule (trapped oil)
in³
psi
grip — Workpiece
73.8 ft·lbf · 1,879 psi
Operating oil pressure 5,802 psi (charged at 5,802, welded ends)
Lift-off ≈ 0 psi · LIFTED floating on 5,802 psi
Sleeve OD +0.001 · Arbor body Ø −0.0001 ΔØ in vs seated
Grip above (joint 2): 1,879 psi · 73.8 ft·lbf
min SF 3.24 at this pressure
in
ft·lbf
The knob is the charge pressure sealed in at assembly. Pressurized oil bulges the thin sleeve as a free ring: it closes the (negative-interference) fitting clearance to the gripped part, and everything past lift-off becomes grip — the contact lines above show the pressure and the torque it holds. The trapped volume sets the oil-spring stiffness: pressure swings with temperature (oil β ≈ 0.0007/°C — roughly K·β ≈ 1.3 MPa or 180 psi per °C when rigidly contained) and with squeeze from outside loads; the Fit-vs-temperature tab re-solves it at every point. Switch OD ↔ ID grip up top to flip which side of the sleeve does the work.
The fit
Joint 1 Arbor body ↔ Sleeve · Ø 1.1 in
in
Preset
in
Joint 2 Sleeve ↔ Workpiece · Ø 1.26 in
in
Preset
in
Joint fits for the capsule build — grip clearances are negative interference; the oil pressure closes them. The grip itself is set by the charge knob below.
Operating loads
psi
psi
rpm
°F
Model
hot bore → cooler surface adds thermoelastic stress; replaces uniform temps while on.
3 · Sleeve 3-D stress field — pressure band, press-fit lands, workpiece
Rating A · max oil p — no part, SF ≥ 1.5
8,653.2 psi
Rating B · joint torque — part on
18.7 ft·lbf
land press fit governs
Pressure band Lp
in
Land press fit Ø
in Ø
End welds
Workpiece length
in
Both ratings live here: A charges the bare sleeve to the SF floor (worst stress — nothing restrains the bulge), B reads the torque paths with the part mounted and deflecting. SF floor comes from the hydraulic panel above.

Lift ΔØ along the sleeve: the band bulges, the lands sit on the press line until the oil peels them, the workpiece caps the lift at its clearance. Thick overlays mark live contact.

von Mises at the two wall faces along the sleeve — the band-edge bending spike and the weld clamping moment are the 3-D effects a uniform-section solve cannot see.

Condition A — no workpiece: max oil pressure at SF ≥ 1.58,653.2 psi (charge ≈ 8,653.2 psi)
bare sleeve at the current chargepeak vM 42,292 psi at the band edge · SF 2.25
Condition B — workpiece mounted: grip on Workpiececontact 1.09 in · mean 1,745 psi · 47.3 ft·lbf
sleeve→body path (seated lands)0.28 in seated per land · mean 1,729 psi · 18.7 ft·lbf
joint rating (weaker friction path; welds in reserve)18.7 ft·lbf — land press fit governs
with the part on: peak vM27,919 psi · SF 3.4
ends (both welded) & axialNx 81.63 kN/m tension · end close-in 0.00002 in Ø vs seat · boundary layer 1/β ≈ 0.17 in
Oil at 5,801.5 psi operating (charge 5,801.5 psi, trapped-oil re-solve) over Lp 1.18 in. The gauges and grip tiles above run the exact N-layer engine with full-length uniform contact; this panel resolves the axial dimension, so its footprint and torque are the smaller, honest numbers — let them govern.
4 · The sleeve in 3-D — von Mises field on the deformed body
Drag to orbit · scroll to zoom. The cutaway shows the through-wall field; the skins carry the face stresses. Deformation exaggerated ×65. Pe — static preview; the interactive view loads with JavaScript.

Drag to orbit · scroll to zoom. The cutaway shows the through-wall field; the skins carry the face stresses. Deformation exaggerated ×65. Peak vM 27,919 psi vs σy(sleeve) 95,000 psi — re-solved live at every knob turn.

5 · Principal-direction field — σ1 arrows through the wall
Drag to orbit · scroll to zoom. Each arrow lies along the local σ1 (most-tensile principal) direction; length tracks |σ1| and color its sign — static preview; the interactive view loads with JavaScript.

Drag to orbit · scroll to zoom. Each arrow lies along the local σ1 (most-tensile principal) direction; length tracks |σ1| and color its signed level — tension vs compression. Hoop rings where ring stretch rules; near welds and band edges the bending + transverse-shear tilt rotates the arrows into the wall. Geometry undeformed. σ1 spans 10,484 … 27,322 psi — re-solved live at every knob turn.

I · In-plane field (Airy). Axisymmetric plane elasticity derives from the Airy stress function φ(r): σr = φ′/r, σθ = φ″, with ∇⁴φ = 0. The single-valued axisymmetric biharmonic is φ = A ln r + C r² (the r²ln r term is dropped — it carries a multivalued displacement), which is exactly Lamé’s field: σr = A/r² + 2C, σθ = −A/r² + 2C. Fixing A, C from the face pressures and integrating Hooke’s law gives every stiffness this panel uses: the sleeve’s own ring stiffness ks = Et/R̄² (thin limit) and the one-sided springs of the body and the workpiece (bore-loaded ring: k = E/{Ri[(Ro²+Ri²)/(Ro²−Ri²)+ν]}; OD-loaded: same bracket with −ν at Ro; solid shaft: k = E/[R(1−ν)]).

II · Axial structure. Let w(x) be the radial motion of the sleeve wall. Its energy per unit circumference is ∫[ ½D(w″)² + ½ksw² − q w ]dx with the plate rigidity D = Et³/12(1−ν²); stationarity gives the cylindrical-shell equation D wⅣ + ksw = q(x) — a beam on the Airy-derived elastic foundation. Disturbances heal over 1/β with β = [3(1−ν²)]¼/√(R̄t); under the band the particular solution is the membrane lift wm = pR̄²/Et.

III · Edge redundants by Castigliano. A semi-infinite shell end-loaded by (P, M₀) stores U = (β/ks)[P² + 2βPM₀ + 2β²M₀²], so ∂U/∂P and ∂U/∂M₀ hand over the end influence coefficients. Splitting the band step into a uniform half (no bending) plus an antisymmetric half (w = w″ = 0 at the step) proves the step transfers by pure shear: M(edge) = 0, w(edge) = wm/2 exactly, Q₀ = kswm/4β, with peak band moment (p/4β²)e−π/4sin(π/4) and the “ends close in” dip −0.0335 wm at βη = 3π/4 just outside the band. Pressure running to a welded end instead gives the classic clamp moment |M₀| = p/2β² and shear p/β.

IV · One-sided contacts. The lands obey qb = kbb−w) ≥ 0 (press fit that can peel, never pull) and the part qp = kp(w−c) ≥ 0 over its length — a linear complementarity problem on the shell operator, solved by an active-set iteration (loads and springs are weighted by Rface/R̄ so face line-loads map correctly to the midsurface). The welds tie the sleeve to the seated line and, because hoop tension Poisson-shortens the tube, pick up an axial force Nx = νEt mean(w)/[(1−ν²)R̄] from the closure ∫εxdx = 0.

IV-b · End conditions — the three BVPs. The variation δΠ leaves the boundary terms [D w″·δw′] and [−D w‴·δw], so each end must take either the essential pair (w = wseat, w′ = 0 — a weld) or the natural pair (M = −D w″ = 0, Q = −D w‴ = 0 — an unwelded end). Both welded: essential at ±L/2; the weld pair reacts the Poisson shortening, Nx = νEt mean(w)/[(1−ν²)R̄]; pressure reaching a weld shows the p/2β² clamp moment. One welded: essential at one end, natural at the other; the clamp signature appears on the welded side only, the free side carries the pure membrane (w = wm exactly under uniform pressure), and Nx = 0 — a single weld has no partner to react the couple. No welds: natural at both ends — a uniformly pressurized free-free tube has no boundary layer at all, and the press-fit lands alone retain the sleeve (axially by friction, unmodeled — verify separately). Each case is gated in engine/test_sleeve.js Case 9: the free-free membrane to 10−11, the one-weld clamp to 2%.

V · 3-D stress recovery. σx(x,z) = Nx/t + 12M(x)z/t³; σθ(x,z) = Ew/R̄ + νσx; σr interpolates the face tractions through the wall; von Mises of the triple governs. Every closed form above gates the numerical solver in engine/test_sleeve.js (step transition to 0.2%, clamp moment to 2%, seated land = Lamé series springs to 0.1%, Clapeyron energy balance to 1%, thick-wall engine cross-checks to ≤8%). References: Timoshenko & Woinowsky-Krieger ch. 15; Hetényi, Beams on Elastic Foundation; Den Hartog, Advanced Strength of Materials; Roark ch. 13; Timoshenko & Goodier for Part I. The full write-up ships with the project as docs/hydraulic-sleeve-derivation.md.

InterfaceØ (in)Interf. Ø (in)Pressure (psi)Assembly force (lbf)Torque (ft·lbf)
1 sealed oil1.10205,801.500
21.26-0.00081,879.41,405.773.8
LayerHoop @ID (psi)Hoop @OD (psi)Max von Mises (psi)Safety factorStatus
1-5,801.5-5,801.52,447.531.41elastic
227,666.723,744.629,344.13.24elastic
33,373.71,494.24,560.47.95elastic
Enable Elastic-plastic analysis in the Model knobs to see the post-yield state here.
Extra gap for an easy slide-on.
convection h for the time-window estimate.
InterfaceHeat outer ΔTor Cool inner ΔT
1+104 °F (→172)−112 °F (→-44)
2+0 °F (→68)−0 °F (→68)
Assembly working window — time before the heated/cooled part drifts back and the gap closes (lumped-capacitance, h≈10 W/m²K):
InterfaceHeat hub: windowCool shaft: window
1
2
Uniform operating temperature applied to all members (assembly ref 20°C). Differential expansion shifts the effective interference — watch for clearance (grip lost) or a falling safety factor.
Operating T (°F)Min contact p (psi)Min SFStatus
-220clearance
320clearance
860clearance
1400clearance
1940clearance
2480clearance
3020clearance
3560clearance
4100clearance
4640clearance
5180clearance
Run a Wall study from the Hydraulic expansion knobs to compare sleeve thicknesses here.

Notes

Engine: N-layer compound-cylinder solver (Lamé thick-wall, multi-interface coupled solve via Eigen, compiled to WebAssembly). Contact is unilateral — an interface flagged clearance has separated under the given loads/temperatures. Safety factor = material yield ÷ peak von Mises (set σy via the material). Suggested-fit limits use the ISO 286 tables from the source workbook; validated to <0.1%.
Elastic-plastic analysis (opt-in, in Loads & options) runs an incremental flow-theory solve (von Mises J2 or Tresca; perfectly-plastic or with linear strain hardening set per material via a tangent modulus Et) for the true post-yield state: it caps stress at the yield surface, grows a plastic zone from the bore, relieves the contact pressure, and reports the residual stress and the gross-yield (limit-load) margin — the factor by which the whole load can scale before a member becomes fully plastic, found numerically. The standard first-yield safety factor remains a valid conservative basis; the limit-load margin governs once a member is allowed to yield locally. A fit that exceeds gross-yield collapse is flagged.
The hardening model chooses how a hardened material re-yields when the operating loads are removed: isotropic grows the yield surface (reverse yield delayed by the full 2·(σy+Et-growth) span), while kinematic translates it — the Bauschinger effect, so reverse yield follows a fixed 2·σy swing and re-yields earlier, eroding the locked-in autofrettage compression. The two coincide on monotonic loading and whenever Et=0; the difference appears only on reverse yielding, which the panel flags. Kinematic/mixed applies to the von Mises criterion (the standard Prager back-stress calibration).

How It Works

A hydraulic arbor is an interference fit you can switch on and off. A thin sleeve is welded to the body around an annular oil chamber; a setscrew piston (or a factory charge) pressurizes the trapped oil and the sleeve bulges elastically as a free ring — a few hundredths of a millimetre is plenty. That motion closes the small fitting clearance to the part, and every bit of pressure past lift-off becomes contact pressure at the grip; friction riding on that pressure holds the torque, exactly the thick-wall (Lamé) mechanics of a press fit. This page runs the same N-layer engine as the Press-Fit Designer with the oil film as one more unilateral interface — OD grip puts the chamber under the sleeve so it expands into a workpiece bore (expanding arbor / mandrel); ID grip puts the chamber outside the sleeve so it contracts onto a tool shank (expansion chuck). Because the ends are welded, the oil is a closed spring: temperature and outside squeeze re-solve its operating pressure through the trapped volume.

Key Components

Common Configurations

Advantages and Limitations

References & further reading

Disclaimer

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